Dynamic Response Analysis of Bird Strike on Aircraft Windshield Based on Damage-modified Nonlinear Viscoelastic Constitutive Relation (P)
CHINESE JOURNAL OF AERONAUTICS ; 20 , 6 ; 511-517
2007-01-01
7 pages
Article (Journal)
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Windshield Bird Strike Structure Design Criteria
NTIS | 1973
|High-Speed Bird Impact Analysis of Aircraft Windshield by Using a Nonlinear Viscoelastic Model
British Library Conference Proceedings | 2013
|FE Analysis of Dynamic Response of Aircraft Windshield against Bird Impact
Tema Archive | 2013
|FE Analysis of Dynamic Response of Aircraft Windshield against Bird Impact
DOAJ | 2013
|USAF Aircraft Windshield/Canopy Bird Strikes
NTIS | 1983
|